EFIS-D100 Electronic Flight Information System - Dynon Avionics

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EFIS Operation Abbreviation Display Item Function CRS Course Pointer Toggles the display of a “V”-shaped course pointer on the heading tape. Like the CDI, this can only be displayed when the EFIS-D100 is receiving a valid course from the NAV source selected on the HSI page. If the CRS button status displays “Y” and no course pointer is displayed on the heading tape, the EFIS-D100 cannot detect your NAV radio or GPS, there is no active course set, or there is no NAVSRC chosen. TRIM Elevator Trim Displays the elevator trim. This can only be displayed when an elevator trim sensor is properly connected to a DSAB-connected EMS device, and configured in the EMS setup. CHECK FIRMWARE VERSION The EFIS > SETUP > VRSION menu gives you two important pieces of information: your EFIS-D100’s current firmware version; and the number of hours the EFIS-D100 has been on. If you require technical support or other assi stance from Dynon, please have your firmware version ready when you call or write. INFO – Informational Items In the EFIS > INFO menu, you have the option of displaying an informational display item on either the left or right side, or both. You may display a voltmeter (VMETER), g-meter (GMETER), vertical speed indicator (VSI), OAT/true airspeed/ density altitude (OAT), and engine RPM/MAP info (ENGINE). More detail about each of these is given below. Voltmeter EFIS-D100 Pilot’s User Guide 5-11
EFIS Operation The voltmeter displays 3 rows of information corresponding to the three power inputs on the EFIS- D100. The first row, labeled M, displays the Master Switch voltage. The second row, labeled E, displays your optional external backup voltage. The third row, labeled I, displays the EFIS-D100 internal battery voltage. If any of the 3 voltage inputs are not present, 00.0V is displayed for the respective voltage values. The letter V follows all three values, denoting the fact that voltages are being displayed. The EFIS-D100 alerts you when the internal battery is low by displaying a low battery alert. G-meter The g-meter displays the current vertical acceleration experienced by the EFIS-D100 measured in g’s, where 1 g is the amount of acceleration due to the earth’s field experienced by an object at sea level. Positive g-force is defined as upward vertical acceleration, making you feel heavier. Negative g-force is defined as downward vertical acceleration, making you feel lighter. As can be seen in the picture, there are three rows of text that make up the g-meter. The top row, labeled MX, is the maximum positive g-force experienced by the EFIS-D100 since reset. The middle row, labeled CR, is the current g-force experienced by the EFIS-D100. The bottom row, labeled MN, is the minimum g-force experienced by the EFIS- D100 since reset. To reset the max and min g-force values to the current g-force value, enter the EFIS > INFO menu button. VSI (Rate of Climb) and press the RSET G The vertical speed indicator (VSI) consists of a single line with your current rate of climb or descent. If you are currently gaining altitude, an up arrow is displayed to the right of the vertical speed value. If you are losing altitude, a down arrow is displayed to the right of the vertical speed value. The units of VSI are feet/minute. Note that in the MODERN display (EFIS > SETUP > STYLE), found in EFIS- D100 firmware version 3.0 and higher, VSI can be displayed as a graphical indicator next to the altitude tape. 5-12 EFIS-D100 Pilot’s User Guide
Page 1 and 2: EFIS-D100 Electronic Flight Informa
Page 3 and 4: Introduction Information in this do
Page 5 and 6: Table of Contents Menu Pages.......
Page 7 and 8: 1. INTRODUCTION Thank you for purch
Page 9 and 10: Introduction The following icons ar
Page 11 and 12: Product Overview SENSORS AND INPUTS
Page 13 and 14: Product Overview GPS Pitot Static A
Page 15 and 16: 3. PRODUCT OPERATION After reading
Page 17 and 18: Product Operation The EFIS-D100 has
Page 19 and 20: Changing the Screen Rotation Produc
Page 21 and 22: Product Operation Pressing a button
Page 23 and 24: 4. AVAILABLE PAGES The EFIS main pa
Page 25 and 26: Horizon line, pitch and roll indica
Page 27 and 28: Turn rate indicator Available Pages
Page 29 and 30: Available Pages the AOA display. To
Page 31 and 32: Available Pages Autopilot Status In
Page 33 and 34: Available Pages Lists Pages Availab
Page 35 and 36: EFIS Operation The BARO setting can
Page 37 and 38: EFIS Operation The airspeed bug can
Page 39 and 40: EFIS Operation you display a checkl
Page 41 and 42: EFIS Operation In a DSAB network, y
Page 43: EFIS Operation Abbreviation Display
Page 47 and 48: EFIS Operation All screens in a DSA
Page 49 and 50: EFIS Operation “all data” and
Page 51 and 52: HSI Operation All HSI screens in a
Page 53 and 54: HSI Operation 6. Winds aloft. This
Page 55 and 56: HSI Operation 6. Glideslope flag. T
Page 57 and 58: HSI Operation 4. To indicator. Ther
Page 59 and 60: HSI Operation BUG - This is the sam
Page 61 and 62: Autopilot Operation normal business
Page 63 and 64: Autopilot Operation AP Status Indic
Page 65 and 66: Autopilot Operation HDG: HEADING MO
Page 67 and 68: Autopilot Operation ALT: ALTITUDE M
Page 69 and 70: Autopilot Operation (HDG, TRK, or
Page 71 and 72: Autopilot Operation AP Button: When
Page 73 and 74: Autopilot Operation FIRST ACTION mo
Page 75 and 76: Autopilot Operation HOLD TO ENGAGE
Page 77 and 78: 8. ALERTS Alarm Indicators Any time
Page 79 and 80: Multiple Alarms Alerts Any time mul
Page 81 and 82: 9. APPENDIX This appendix contains
Page 83 and 84: Appendix Start Width Description No
Page 85 and 86: Alert Message Description End condi
Page 87 and 88: Alert Message Description End condi
Page 89: Appendix Inputs/Outputs 1 - Audio A

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